I consider the entire model engine intake assembly (before the crankshaft) to simply be a fuel/air metering device that has very little atomization capabilities. (And the more you try and chase atomization capabilities the more inconsistent it becomes in a changing stunt environment.)
Witness the fact that one can run an engine on a burst just by priming it with straight fuel, no droplets, no atomization, just a small solid volume of fuel as most of the atomization occurs much later in the exit of the transfer ports - e.g. small ports give high speed and far better flow and atomization just like miniature low pressure fuel injectors.
Thus one should look at how well any stunt venturi system will give a consistent metering of sheared droplets and not bother even considering how fine the resultant spray is going to be.
Atomization is absolutely critical to reliable stunt runs. David and I have experimented a lot with both the fuel feed and the air intake over the past 10 or so years, following on to Frank Williams' experiments with spigot venturis. Contrary to the laminar flow or pressure recovery theories, the most reliable and consistent runs come from venturis with the most turbulent flow, and even something like the panty hose diffuser/filter can make a marked difference in the run quality. The first example was the astonishing improvement in the inside/outside speed variation by switching to a spigot venturi just exactly like Frank's article on the topic. If we hadn't solved that I would still be running 40VFs.
I am pretty convinced that despite the fact that it might flow better on a bench, the very last thing you want is anything like streamlined flow and you certainly do not want the charge flow attaching to the walls and just dribbling into the engine. Sergei Belko's "top intake" engine is intriguing because it allows you to use the entire nose of the airplane as an airbox or plenum. I think that's why the original ST sprinkler venturi worked better than a lot of the later "flush inlet" types, even if you drill out the seat where the sprinkler holes are. There are a few sharp edges right upstream of the holes that certainly break up any notions of laminar flow.
There's a few long threads on this topic in the archives on SSW, but we have gotten smarter since then. And I am sure our mavens for rigor will be down on me for the rampant speculation and anecdotal evidence shown here.
The other thing that appears to make a huge difference is how the fuel supply path works, and the viscosity and flow characteristics of the fuel itself. The flow rate is pretty slow ON AVERAGE, but it's not constant so the the peak flow rates can apparently be pretty high. This we learned from both Brian Eather's observations on fuel viscosity and the early problems with 4-strokes on overheads. One of the keys, with a remarkable improvement, was switching (at Brad Walker's suggestion at the 2002 NATs, probably originally from Bill Wilson and RC guys) to a clunk tank. That led to looking at what was going on with fuel flow.
Some of what found on the fuel path is still semi-secret, sorry about that, because I didn't invent it and it has not been published. I am sure that there will be 5 people claiming that they know what we are doing, they originally invented it, and we're stupid, but that's the way it goes sometimes. For the most part, reduce the flow restriction to the extent possible even if it seems pointless and works OK the way it is now. But don't make the spigot itself too big, anything downstream of the needle needs to be small enough to stay wetted all the way across the tube. If it's too big after the fuel is metered, it's possible to get the fuel flowing down one side and air coming in the other side. That's probably OK if it stayed that way all the time and never changed, but it will.
Brett